Application of higher-order structural theory to bending and free vibration analysis of sandwich plates with CNT reinforced composite facesheets
Source abstract
Abstract
In this paper, the bending and free flexural vibration behaviour of sandwich plates with carbon nanotube (CNT) reinforced facesheets are investigated using QUAD-8 shear flexible element developed based on higher-order structural theory. This theory accounts for the realistic variation of the displacements through the thickness, and the possible discontinuity in slope at the interface, and the thickness stretch affecting the transverse deflection. The in-plane and rotary inertia terms are considered in the formulation. The governing equations obtained using Lagrange's equation of motions are solved for static and dynamic analyses considering a sandwich plate with homogeneous core and CNT reinforced face sheets. The accuracy of the present formulation is tested considering the problems for which solutions are available. A detailed numerical study is carried out based on various higher-order models deduced from the present theory to examine the influence of the volume fraction of the CNT, core-to-face sheet thickness and the plate thickness ratio on the global/local response of different sandwich plates.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Structural Analysis and Optimization · Nonlocal and gradient elasticity in micro/nano structures
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (22)
Show source-provided references
1. Stress analysis of thick laminated composite and sandwich plates10.1177/002199837200600401 ↗
2. A comprehensive analysis of functionally graded sandwich plates: Part 1 – Deflection and stresses10.1016/j.ijsolstr.2005.02.015 ↗
3. Ugale V, Singh K, Mishra N. Comparative study of carbon fabric reinforced and glass fabric reinforced thin sandwich panels under impact and static loading. J Compos Mater. http://dx.doi.org/10.1177/0021998313514874.10.1177/0021998313514874 ↗
4. Tjong · 2009
5. A comparison of the mechanical properties of fibers spun from different carbon nanotubes10.1016/j.carbon.2010.11.054 ↗
6. Aligned multi-walled carbon nanotube-reinforced composites: processing and mechanical characterization10.1088/0022-3727/35/16/103 ↗
7. Vibrations of carbon nanotube-reinforced composites10.1016/j.jsv.2009.11.020 ↗
8. Static and free vibration analyses of carbon nanotube-reinforced composite plates using finite element method with first order shear deformation plate theory10.1016/j.compstruct.2011.11.010 ↗
9. Nonlinear vibration of nanotube-reinforced composite plates in thermal environment10.1016/j.commatsci.2011.03.005 ↗
10. Buckling analysis of laminated composite rectangular plates reinforced by SWCNTs using analytical and finite element methods10.1007/s12206-011-0127-3 ↗
11. Postbuckling of carbon nanotube-reinforced functionally graded cylindrical panels under axial compression using a meshless approach10.1016/j.cma.2013.09.001 ↗
12. Buckling analysis of functionally graded carbon nanotube-reinforced composite plates using the element free kp-Ritz method10.1016/j.compstruct.2012.11.006 ↗
13. Eshelby–Mori–Tanaka appraoch for vivibration behavior of continuously graded carbon nanotube-reinfroced cylindrical panels10.1016/j.compositesb.2012.01.004 ↗
14. A new theory for accurate thermal/mechanical flexural analysis of symmetrically laminated plates10.1016/S0263-8223(99)00028-8 ↗
15. Free vibration analysis of multi-layered composite laminates based on an accurate higher-order theory10.1016/S1359-8368(01)00028-2 ↗
16. Dynamic analysis of laminated composite plates subjected to thermal/mechanical loads using an accurate theory10.1016/S0263-8223(00)00133-1 ↗
17. Bending and vibration of functionally graded material sandwich plates using an accurate theory10.1016/j.finel.2012.03.006 ↗
18. Nonlinear vibration and bending of sandwich plates with nanotube-reinforced composite fnonlinear10.1016/j.compositesb.2011.04.040 ↗
19. Laminated composite plate theory with improved in-plane responses10.1115/1.3171828 ↗
20. Radial basis functions-finite differences collocation and a unified formulation for bending, vibration and buckling analysis of laminated plates according to Murakami’s zig-zag theory10.1016/j.compstruct.2011.01.009 ↗
21. Free vibration analysis of laminated plates using a layerwise theory10.2514/3.11933 ↗
22. Analysis of composite plates using a layerwise deformation theory and multiquadratics discretization10.1080/15376490490493952 ↗